10.1 Introduction
Validation against analytical solutions, experiments, and real incidents is the preferred way of documenting the range of scenarios for which a model system generates reliable estimates for relevant physical phenomena. Systematic validation is also essential for quality assurance: continuously monitoring the effects of changes in source code, compilers, operating systems. As such, Gexcon has implemented an automated framework for validation of the FLACS-CFD software. Currently, there are approximately 60 validation series included in the automated framework, with approximately 2,700 FLACS-CFD simulations (including a range sensitivity simulations). The cases range from small scale basic verification cases to large scale dispersion and explosion cases.
In this section, a small subset of the validation cases is presented as Validation Summary Sheets to highlight the validation status of FLACS-CFD.
10.2 Structure of Validation Summary Sheets
The validation results are presented as succinct validation documents (Validation Summary Sheets) that clearly communicate the FLACS-CFD performance for particular test cases.
10.2.1 Experiment details
The first page of the Validation Summary Sheet is used primarily to present the details of the experiment, highlighting the relevance for FLACS-CFD validation.
10.2.2 FLACS-CFD simulation results
10.2.2.1 Performance metric parameters
Five performance metrics are provided for each campaign. These are
• the geometric mean bias (MG),
MG = exp(lnXp - EXO) (10.1)
• the geometric variance (VG),
VG = exp[(lnXp - lnXO)2] (10.2)
• the fraction of predictions within a factor of two of observations (FAC2),
0.5 < Xp < 2.0 (10.3)
Xo
• the fractional bias (FB), and
FB
Xp - Xo 0.5(Xp + Xo)
(10.4)
• the normalized mean square error (NMSE).
NMSE = (Xp二 Xo)2 (10.5)
XpXo < /
where Xp are the model predictions, X。and the observations and the overbar (e.g. Xo) is the average over the dataset. The number of data points used to calculate each metric (N) is also shown. Bounds are provided for each performance metric to show how they vary across the grid sizes considered for each validation exercise.
A perfect model would have MG, VG, and FAC2 = 1.0; and FB and NMSE = 0.0. Of course, there is no such thing as a perfect model. The individual performance metrics are coloured green if they fall in what is generally considered the acceptable range, i.e.:
• The fraction of predictions within a factor of two of observations is at least 50% (i.e. FAC2 > 0.5).
• The mean bias is within a factor of 2 of the mean (i.e. -0.67 < FB < 0.67 or 0.5 < MG < 2).
• The random scatter is about a factor of two to three of the mean (i.e. NMSE < 1.5 or VG < 4).
Note the above ranges are indicative only. Multiple performance measures should be applied and considered in any model evaluation exercise, as each measure has advantages and disadvantages and there is not a single measure that is universally applicable to all conditions.
10.2.2.2 Performance plots
Two plots types are shown to aid evaluation of model performance; parabola plots and scatter plots. Figures 10.1 and 10.2 present some examples of the scatter plots and their corresponding parabola plots.
10.3 Validation cases
Two-pagers for 50 experimental campaigns are presented, including two new cases for pool fires. A list of the cases is given under each subsection.
10.3.1 Discussion
All validation cases have been run with grids within the grid guidelines. Refer to section ”Recommended grid configuration” for discussion about the grid guidelines and a grid sensitivity assessment. To represent the much more rapid progression of detonation and have a consistent approach across both deflagration, DDT and detonation cases, we have reduced the averaging time of pressure to 0.1ms for the experimental results in all explosion cases (from 1.5ms previously). For deflagrations this is more conservative and may result in slightly increased underprediction in some of the validation cases, as the typical timestep in FLACS-CFD simulations will be longer than this. As the applied averaging time is different, validation performance cannot be exactly compared with previous validation, although in most cases the difference will be modest.
(a) Scatter plot, Xp = X。
(b) Parabola plot, Xp = X。
(c) Scatter plot, Xp > X。
(d) Parabola plot, Xp > X。
(e) Scatter plot, Xp < X。 (f) Parabola plot, Xp < X。
Figure 10.1: Examples of idealised data variation (low scatter) presented in scatter and parabola plots.
• ETHANE. METHANE
• HYDROGEN. METHANE
• ETHYLENE
• METHANE, PROPANE
• METHANE
PROPANE
• HYDROGEN
* MTOROGEK. N2
• BUTMIEr ETHANE. METHANE, PEhTMNE, PR0P4NE ETHANE. METHANE, PROPANE
• BUUNL PROMNE
• METHANE
• COZ, PROPANE
• HYDROGEN
• ETHANE. METHANE, N2
• BENZENE, N_BU7ANE. N.HEXANE, N_PEN1ANE. N_PROPYLBENZENE, 0.XYLENE. TOLUENE
• PROPANE
ETHANE. HYDROGEN, METHANE. N2
Experiment [kW/m2]
Explosion (top-left), Dispersion (top-centre) and Fire (top-
Table 10.1: Gas explosion validation cases.
10.3.2 Gas Explosion
Figure 10.3 (top-left) summarizes the presented explosion validation cases in a single scatter plot, while table 10.1 gives a summary of the individual experiments.
Performance is generally good, though we do see a spread in the results. There is a tendency for FLACS-CFD to perform better for large-scale experiments. This is because experiments at smaller scales are more sensitive to the modelling of quasi-laminar flame propagation and to radiative and convective heat losses. Different mixtures are included in the validation and the performance across different gas species is generally good. However, there are some cases of poor representation of very fast flames; for example, propane and ethylene overpressures are under-predicted. The under-prediction is especially evident for the ethylene cases. FLACS-CFD does not capture the flame instability types that become important at very high flame-speeds (approaching DDT), so the deviations in the results for propane and ethylene are somewhat expected.
In the performance plots, detonation cases are distinguished using a different marker style, as shown in the plot legend. Those are the hydrogen-explosion tests for which detonation was observed in the experiment. In the validation, FLACS-CFD is run with default settings for detonation (DDT ”AUTO” and DDT TIME -1), meaning that detonation is triggered for hydrogen explosions only when DPDX exceeds 1.
In addition to the validation against experimental data, the result of which is presented in the following subsections, FLACS-CFD version 22.2 has been tested for hydrogen explosion using a set of realistic fullscale scenarios. Simulations indicate a higher frequency of detonation events compared to the detonation frequency obtained in the simulation of hydrogen explosion validation cases. For hydrogen-explosion, thanks to the new detonation model in FLACS-CFD version 22.2, on average the user should expect an increase of predicted peak pressure of about 20% compared to the peak pressure obtained from simulating the same scenarios with version 22.1.
10.3.2.1 3D Corner Small Scale
HYDROGEN, N2
Small scale hydrogen explosion experiments were performed in 3D-corner tests (an obstacle array of 37x37x37cm that is blocked on 3 sides and open on 3 sides). The tests considered 3 different obstruction densities, 2 ignition locations, and a range of H2 concentrations.
Location: Gexcon AS (NORWAY)
Year: 2004
Number of cases in series: 32
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 23 mm
REFERENCES
[1]Renoult, J. & Wilkins, B. (2004), Hydrogen explosion safety phase 2 – small scale explosion experiments., Gexcon AS. Report number
GexCon-3-F46201-2
FUEL
HYDROGEN
HYDROGEN, N2
Pressure
N MG
87
36
2.7
2.9
VG
6.1
7.7
FAC2 0.31 0.33
FB
0.59
0.64
NMSE
1.6
2
3UUQ_」P> UC^EO^O
123 2.8 6.6 0.32 0.6
10.0
7.5
5.0
2.5
1.7
Geometric mean bias
〔PBql uoqp-nlu-s
• HYDROGEN, N2
• HYDROGEN
• Detonation
X Deflagration
5 10
Experiment [barg]
10.3.2.2 Bakerrisk
HYDROGEN, ETHYLENE
A set of large-scale unconfined vapor cloud explosion tests were performed in a congested region. The test rig consisted of cubic sections with 1.8 m long tubes located vertically serving as obstacles. Ethylene-air mixtures with concentration varying from lean to rich and lean hydrogenair mixtures were tested. The mixtures were ignited at the centre of rig just above the ground level. Pressure measurements were made using arrays of pressure gauges placed up to 91 m away from the rig [1][2].
Location:
Year:
Number of cases in series: 4
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 120 mm
REFERENCES
[1]Kelly Thomas, Quentin Baker, Don Ketchum, Martin Goodrich, Max Kolbe (2003), Deflagration to Detonation Transition in Unconfined Vapor Cloud Explosions
FUEL
HYDROGEN ETHYLENE
N MG
1.2
5.2
Pressure
VG
FAC2 0.67
FB
-0.065
1.4
NMSE 0.31 3.4
2.4 0.6
0.35
①:}up_」9> :>-」l① LUO ①0
10° ; id-1
All fuels 10 1.4
4 3 2 1 0Bq】 UOA-nLU-s
-0.063
• ETHYLENE
• HYDROGEN
• Deflagration
X Detonation
10°
io1
2 4
Geometric mean bias
Experiment [barg]
10.3.2.3 BFETS Phase 2B
ETHANE, METHANE, PROPANE
Phase 2B of the Blast and Fire Engineering Project for Topside Structures (BFETS) considered large-scale experiments in a test vessel with an internal volume of 50 m3. The vessel included varying geometric congestion and confinement. Experiments were conducted to study the effect of variation in gas concentration, ignition location, and water spray.
Location: Spadeadam, United Kingdom
Year: 1994
Number of cases in series: 14
SELECTION OF TESTS
Available measurements: Flame arrival time, Pressure
SIMULATION SETUP
Grids used: 500 mm
REFERENCES
[1]Evans, J.A., Johnson, D.M. & Lowesmith, B.J. (1999), Explosions in full offshore module geometries (Work carried out under controct to the HSE, MaTSU/8847/3522), BG Technology. Report number R2422
[2]Foisselon, P., Hansen, O.R. & van Wingerden, K. (1998), Detailed analysis of FLACS performance in comparison to full-scale experiments,
Christian Michelsen Research
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL N MG VG FAC2 FB NMSE
ETHANE, METHANE, PROPANE 666
^ucrocra> UC^EO^O
o2
1
10° ; 16T
1
1
10°
Geometric mean bias
0 5 0 5 z L L n^ 【s】UOA-nE-s
1.3
0.98
0.24
1 2
Experiment [s]
• ETHANE, METHANE, PROPANE
Pressure
①OUQ_」B> OC^EO^O
o2
10° ; io-1
FUEL
ETHANE, METHANE, PROPANE
1
10°
Geometric mean bias
8
6 4 2 【peq】 co^ra3E~^
N MG VG FAC2 FB NMSE
370 0.53 2.6 0.58 -0.54 1.1
2.5 5.0 7.5
Experiment [barg]
• ETHANE, METHANE, PROPANE
10.3.2.4 BFETS Phase 3A Deluge
ETHANE, METHANE, PROPANE, BUTANE, PENTANE
Tests performed in realistic offshore compressor modules of dimensions 28m x 12m x 8m. The experimental program investigated the degree of congestion (equipment density), degree of confinement (vent area), ignition location, repeatability, and the effect of various water deluge layouts [1] [2][3]. This subset is only the water spray tests, excluding those two tests (tests 28 and 34) with vessel specific deluge.
The deluge tests (35 & 36) do not include th scaffolding.
Location: United Kingdom
Year: 1997 - 2000
Number of cases in series: 19
Available measurements: Pressure
Grids used: 500 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Evans, J.A., Johnson, D.M. & Lowesmith, B.J. (1999), Explosions in full offshore module geometries (Work carried out under controct to the HSE, MaTSU/8847/3522), BG Technology. Report number R2422
[2]Al-Hassan, T. & Johnson, D.M. (1998), Gas explosions in large-scale offshore module geometries: Overpressures, mitigation and repeatability.
[3]Foisselon, P., Hansen, O.R. & van Wingerden, K. (1998), Detailed analysis of FLACS performance in comparison to full-scale experiments,
Christian Michelsen Research
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL
ETHANE, METHANE, PROPANE
BUTANE, ETHANE, METHANE, PENTANE, PROPANE PROPANE
①:}UQ_」P> OCXEO^O
All fuels
【peq】 UOAB-nE-s
N MG VG
384
173
71
0.67
0.87
0.52
1.8
1.2
1.7
FAC2 0.68 0.91 0.66
FB
-0.43
-0.1
-0.63
NMSE
1.8
0.16
0.58
628 0.7 1.6 0.74 -0.39 1.7
Geometric mean bias
2 4
Experiment [barg]
• PROPANE
• BUTANE, ETHANE, METHANE, PENTANE, PROPANE
• ETHANE, METHANE, PROPANE
10.3.2.5 BFETS Phase 3A
ETHANE, METHANE, PROPANE, BUTANE, PENTANE
Tests performed in realistic offshore compressor modules of dimensions 28m x 12m x 8m. The experimental program investigated the degree of congestion (equipment density), degree of confinement (vent area), ignition location, repeatability, and the effect of various water deluge layouts [1] [2][3] .
Location: United Kingdom
Year: 1997 - 2000
Number of cases in series: 9
Available measurements: Pressure
Grids used: 500 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Evans, J.A., Johnson, D.M. & Lowesmith, B.J. (1999), Explosions in full offshore module geometries (Work carried out under controct to the HSE, MaTSU/8847/3522), BG Technology. Report number R2422
[2]Al-Hassan, T. & Johnson, D.M. (1998), Gas explosions in large-scale offshore module geometries: Overpressures, mitigation and repeatability.
[3]Foisselon, P., Hansen, O.R. & van Wingerden, K. (1998), Detailed analysis of FLACS performance in comparison to full-scale experiments,
Christian Michelsen Research
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
|
FUEL |
N |
MG |
VG |
FAC2 |
FB |
NMSE |
|
ETHANE, METHANE, PROPANE |
291 |
0.7 |
1.7 |
0.75 |
-0.45 |
1.2 |
|
BUTANE, ETHANE, METHANE, PENTANE, PROPANE |
38 |
1 |
1.1 |
0.95 |
0.015 |
0.35 |
|
All fuels |
329 |
0.73 |
1.6 |
0.77 |
-0.39 |
1.1 |
• BUTANE, ETHANE, METHANE, PENTANE, PROPANE
• ETHANE, METHANE, PROPANE
10.3.2.6 BFETS Partial Fills
ETHANE, METHANE, PROPANE
Available measurements: Flame arrival time, Pressure
BFETS PARTIAL FILLS
Location: BG Spadeadam (UK)
Year: 1994
Number of cases in series: 6
REFERENCES
A series of six explosion experiments were conducted. The explosion experiments were conducted in the full-scale explosion rig at BG Spadeadam, which is designed to be representative of an offshore module [1][2]. The experiments studied explosions produced by ignition of a homogeneous mixture of natural gas and air with the volume of the natural gas and air mixture ranging between 10% and 100% of the volume of the explosion rig. The six tests were carried out using a lengthened module of 28m x12m x8m. Variations in the experiments included different gas cloud size without mitigation techniques.
SELECTION OF TESTS
SIMULATION SETUP
[1]Evans, J.A. & Johnson, D.M. (1999), Gas explosions in offshore modules following realistic releases (Phase 3B): Data report for large scale partial fill experiments, BG Technology. Report number GRTC R3245
[2]Johnson, D.M & Cleaver, R.P. (2002), Gas explosions in offshore modules following realistic releases (Phase 3B): Final summary report.
Report number R 4853
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL N MG VG FAC2 FB NMSE
ETHANE, METHANE, PROPANE 374 1.1 1 0.99 0.1 0.032
^ucrocra> UC^EO^O
o2
1
1
1
Geometric mean bias
R>- n^ E^ 1 1 o 【s〕UOA-nE-s
0.5 1.0 1.5
Experiment [s]
• ETHANE, METHANE, PROPANE
Pressure
①OUQ_」B> OC^EO^O
o2
FUEL
ETHANE, METHANE, PROPANE
1
Geometric mean bias
N MG VG FAC2 FB NMSE
127 1.4 1.5 0.65 0.19 0.51
Experiment [barg]
• ETHANE, METHANE, PROPANE
10.3.2.7 DNVGL 180m3
BUTANE, ETHANE, METHANE, PENTANE, PROPANE
Large-scale vented confined explosions conducted at the
Spadeadam Test Site to study the effect of vent size and congestion on vented explosions. Thirty-eight stoichiometric natural gas explosions were carried out in 182 m3 vented explosion chamber. Polyethylene pipes were used to provide congestion with volume blockage ranging from 0% to 5%.
Location: Spadeadam test site, UK
Year: 1991
Number of cases in series: 25
Available measurements: Pressure
Grids used: 225 mm, 300 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Tomlin, G. and Johnson, D.M. and Cronin, P. and Phylaktou, H.N. and Andrews, G.E (2015), The effect of vent size and congestion in large-scale vented natural gas/air explosions, Journal of Loss Prevention in the Process Industries
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
BUTANE, ETHANE, METHANE, PENTANE, PROPANE 53 0.98 – 1.4 1.3 – 1.5 0.77 – 0.83 0.16 – 0.19
0.14 – 0.53
6 4 2 【PQq】 Co^ra-DE-^
IO-1 10° IO1
Geometric mean bias
2 4 6
Experiment [barg]
• BUTANE, ETHANE, METHANE, PENTANE, PROPANE
10.3.2.8 EMERGE
METHANE, PROPANE
The project EMERGE (Extended Modelling and Experimental Research into Gas Explosions) provided a set of experimental explosion data at different scales, for two fuel types, with different obstruction parameters and with turbulence present in the flammable mixture at ignition. The geometry was similar to the MERGE project (the experiments of involved a single array of pipes).
Location: British Gas Fauld and Spadeadam test facilities (UK)
Year: 1996
Number of cases in series: 12
Available measurements: Pressure
Grids used: 150 mm, 300 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Shale, A.G. & Walker, D.G. (1996), Extended Modelling and Experimental Reseach into Gas Explosions (EMERGE) - Final report for medium and large scale explosion experiments. Report number R1327
FUEL METHANE PROPANE
N 18 30
Pressure
MG 0.74 – 0.89 0.62
All fuels 18 0.74 – 0.76
IO"1 10°
Geometric mean bias
VG
1 – 1.1
1.4
FAC2
1 0.77
1.1 – 1.2 0.89 – 1
〔PQq〕UOQCnE-s
2.5
2.0
1.5
1.0
0.5
FB -0.3 – -0.16
-0.68
NMSE 0.049 – 0.098 1.3
0.098 – 0.92
-0.46 – -0.3
• PROPANE
• METHANE
1 2
Experiment [barg]
10.3.2.9 Fh-ICT Lane Experiment
HYDROGEN
The test setup consisted of a driver section that was a rectangular container (3 x 1.5 x 1.5 m). There was a squarespaced opening in the front wall of the driver section with a blocking ratio 0.1 (tests IA1, IA2, IA3) and 0.3 (tests IA4 and IA5). The container was followed by a "lane" which consisted of 2 parallel walls (thickness 4 cm) at a distance of 3 m with a length of 12 m and a height of 3 m. The walls were fixed with steel braces to ensure that they do not move during the experiments. The whole volume was filled with H2- air mixture. The hydrogen mixture was enclosed within the lane using a polyethylene foil (thickness 0.2 mm). The mixture was ignited at the rear side of the container with five distributed pyrotechnic igniters. Two vertical tubes (diameter 14 cm) were installed at a distance of 5 cm from the wall each in the middle and at the end of the lane for all tests except test IA1.
Location: Fraunhofer Institute for Propellants and Explosives (ICT), Germany
Year: 1984
Number of cases in series: 4
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 100 mm
REFERENCES
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
3.5 0.38 0.37 1.3
【PQq】 UOAQ-nE-s
QUG^Cro> u-」4-1山 lu 090
Experiment [barg]
Geometric mean bias
10.3.2.10 Fireseal Pipe Penetration Blast Wall
PROPANE, METHANE
Large-scale tests explosion tests were performed to study the behaviour and explosion blast resistance properties of passive fire protection from FireSeal AB. Standard Gexcon 50m3 module with geometry modifications was used. The main aim was to test the fire seal pipes on blast wall which was mounted using adaptor frame on the Gexcon module. The series of tests included some reference tests to fix the internal geometry layout/configuration that could give the desired explosion loading on the blast wall and pipe setup.
Location: Sutra,Burgen
Year: 11/04/2021 - 25/04/2021
Number of cases in series: 10
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 167 mm
REFERENCES
[1]Brian A. Wilkins (2021), Explosion Testing of FireSeal Pipe Penetrations Seals and Blast Wall
FUEL PROPANE METHANE
N
62
7
Pressure
MG
VG
FAC2
FB
0.72
1
1.4
1
0.73
1
-0.43
-0.0068
NMSE 0.5 0.015
① uuro_」Q> OCSEOQO
0.52
• METHANE
• PROPANE
1 2
Experiment [barg]
10.3.2.11 FM Global 64m3 empty
PROPANE, HYDROGEN, METHANE
The experiments were conducted in an empty 64 m3 chamber with dimensions 4.6m x 4.6m x3m with square vents of 5.4 m2 and 2.7 m2. The fuels used were methane, propane and hydrogen [1][2].
Location:
Year:
Number of cases in series: 18
4.6 m
‘Center
Ignition
Back |
Ignition、^
' ' Front
Ignition
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]Chao, J. Bauwens, C.R. & Dorofeev, S.B. (2011), An analysis of peak overpressures in vented gaseous explosions, Proceedings of the Combustion Institute
[2]Bauwens, C.R. (2010), Effect of ignition location, vent size, and obstacles on vented explosion overpressures in propane-air mixtures, Combustion Science and Technology
Pressure
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Geometric mean bias
Experiment [barg]
10.3.2.12 FM Global 64m3 Obstacles
METHANE, PROPANE
Vented explosion experiments were conducted using stoichiometric methane-air and propane-air mixtures in FM Global's large-scale explosion test chamber. The test chamber had overall dimensions of 4.6 x 4.6 x 3.0 m and an overall volume of 63.7 m3. A square vent with two possible surface areas, either 5.4 m2 or 2.7 m2, was located on one of the chambers vertical walls. The tests were focused on the effect of fuel, enclosure size, ignition location, vent size, and obstacles on the pressure development of a propagating flame in a vented enclosure. The dependence of the maximum pressure generated on the experimental parameters was analysed.
Location: Rhode Island, USA
Year: 2010
Number of cases in series: 10
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]Chao, J. Bauwens, C.R. & Dorofeev, S.B. (2011), An analysis of peak overpressures in vented gaseous explosions, Proceedings of the Combustion Institute
[2]Bauwens, C.R. (2010), Effect of ignition location, vent size, and obstacles on vented explosion overpressures in propane-air mixtures, Combustion Science and Technology
FUEL
METHANE PROPANE
Pressure
VG
2.3
2.3
FAC2 0.17 0.5
FB
0.76
0.54
NMSE
1.6
1.1
① uuro_」Q> 0CSE0Q0
.3 ..... 2 5 4 3 2 1 o.0.0.0.0. 【PBq】 UOA-nE-s
.5
0.3
0.69
0.2
0.4
1.5
PROPANE
METHANE
Geometric mean bias
Experiment [barg]
10.3.2.13 FMGlobal Hydrogen Initial Turbulence
HYDROGEN
The Experiment is conducted in 64 m3 chamber with dimensions 4.6*4.6*3 with square vent of 5.4m2. Fuel used is Hydrogen with different concentration, initial turbulence and ignition location.
Location:
Year:
Number of cases in series: 15
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]Bauwens, C. Regis and Dorofeev, S.B. (2014), Effect of initial turbulence on vented explosion overpressures from lean hydrogen–air deflagrations, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
7.2
.5
87
• HYDROGEN
【peq】 co-^ra-DE-^
IO-1 10° IO1
Geometric mean bias
0.2 0.4
Experiment [barg]
10.3.2.14 FM Global Hydrogen Concentration
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
2
18 0.
.7 3
.9
2
【peq】 co-^ra-DE-^
• HYDROGEN
0.5 1.0
Experiment [barg]
HYDROGEN
22
QUG^Cro> u-」4-1山 lu 090
Geometric mean bias
10.3.2.15 Hydrogen Balloon
HYDROGEN
The experiment consisted of a 20 meters diameter polyethylene hemispheric balloon placed on ground and filled with stoichiometric hydrogen-air. The combustion was initiated by ignition pills at the centre of the hemisphere basement. Pressure dynamics were recorded using 11 transducers, installed on the ground level in a radial direction at distances from 2 to 80 meters away from the centre of the hemisphere basement at radii- R = 2.0, 3.5, 5.0, 6.5, 8.0, 18.0, 25.0, 35.0, 60.0 and 80.0 meters. Flame propagation was evaluated along the radial path between 45deg and 135deg from the point of ignition [1][2].
Location: Germany Year: 1983
Number of cases in series: 1
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 600 mm
REFERENCES
[1]HySafe (2005), SBEP-V2: Fh-ICT Balloon Test
[2]Hansen, O.R. & Storvik, I. (2005), SBEP-V2: Fh-ICT Balloon Test. FLACS-HYDROGEN CALCULATIONS. Report number GexCon-05-F46207-
Tech.Note no2
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①OUP_」B> OC^OEOau
1 1 0.036 0.045
【PQq〕UOAP-nE一s
Geometric mean bias
Experiment [barg]
10.3.2.16 Hydrogen Refueling Station
HYDROGEN
The experiment in a mock-up of a hydrogen refuelling station was conducted jointly by Shell Global Solutions (UK) and the Health and Safety Laboratory (UK) in order to study the potential hazards and consequences associated with a hydrogen-air mixture explosion. The a€reworst-casea€K scenario of a stoichiometric hydrogen-air mixture explosion was offered for this simulation exercise.
Location: Shell Global Solutions (UK)
Year: 2007
Number of cases in series: 1
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 110 mm
REFERENCES
[1]Makarov, D., Verbecke, F, Molkov, V., Roe, O., Skotenne, M., Kotchourko, A., Lelyakin, A.,Yanez, J., Hansen, O., Middha, P., Ledin, S., Baraldi, D., Heitsch, M., Efimenko, A. & Gavrikov, A. (2009), An inter-comparison exercise on CFD model capabilities to predict a hydrogen explosion in a simulated vehicle refuelling environment, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
0.12
HYDROGEN
QUG^Cro> u-」4-1山 LU 090
【PQq】 UOAQ-nE-s
Geometric mean bias
4 3 o.O-
2 o.
• HYDROGEN
0.2 0.3 0.4
Experiment [barg]
10.3.2.17 HySEA Homogeneous
HYDROGEN
66 vented hydrogen deflagration experiments were performed in 20-foot ISO containers. 34 test were conducted with homogeneous and quiescent mixtures. The project objective was to improve the hydrogen safety for energy applications through pre-normative research on vented deflagrations [1][2].
Location: Gexcon AS (NORWAY)
Year: 2016-2018
Number of cases in series: 36
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 100 mm, 153 mm
REFERENCES
[1]Skjold, T. (2018), Vented hydrogen deflagrations in 20-foot ISO containers
[2]Skjold, T., Hisken, H., Lakshmipathy, S., Atanga, G., van Wingerden, M., Olsen, K. L., Holme, M. N., Turøy, N. M., Mykleby, M., van Wingerden, K. (2019), Vented hydrogen deflagrations in containers Effect of congestion for homogeneous and inhomogeneous mixtures., International Journal of Hydrogen Energy
DATE: FEBRUAR 16, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①uup_」e> UC^OEOa^
〔6」pq- uo匚B-nLU-s
• HYDROGEN
25 – 30
Geometric mean bias
Experiment [barg]
10.3.2.18 HySEA Unipi
HYDROGEN
To investigate vented hydrogen explosions in installations such as gas cabinets, cylinder enclosures, dispensers, and backup power systems. The experimental setup allows researchers to study the effect of internal obstacles (bottles), construction materials (including structural response), and the effect of mitigating hydrogen deflagrations by means of various venting devices. Experiments on small scale enclosure additionally provide information on the opening inertia of the vent panel at low hydrogen concentration and on the measurement of the structural response [1][2].
Location: University of Pisa (Italy)
Year: 2017
Number of cases in series: 9
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 90 mm
REFERENCES
[1]Fineschi, F., Landucci, G., Schiavetti, M., Pini, T. & Carcassi, M. (2016), Small-scale enclosure Dimensions and design. Report number HySEA-D-2-01-2016
[2]Fineschi, F., Landucci, G., Schiavetti, M., Pini, T. & Carcassi, M. (2017), Small-scale enclosure. Experimental campaign of hydrogen deflagrations for homogeneous H2 concentrations. Report number HySEA-D-2-03-2017
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①OUP_」B> OC^OEOau
【PQq〕UOAP-nE一s
0.021
• HYDROGEN
Geometric mean bias
Experiment [barg]
10.3.2.19 JIP MEASURE AR8DR8 SD2 SD9
PROPANE
Gexcon AS developed a Joint Industry Project, Modelling Escalating Accident Scenarios and the Use of Risk-reducing technology for Explosion safety (MEASURE), that included the conduction of large scale experiments to provide validation data for explosion modelling (e.g., FLACS-CFD). Here, we consider the tests using a configuration with type 8 congestion (an array of 8x8x4 pipes of 168.3 mm in diameter and 655 mm in pitch, offering approximately 17% volume blockage) for eight different separation distances (SD) [1][2][3].
Location: United Kingdom
Year: 2013-2017
Number of cases in series: 2
SELECTION OF TESTS
Available measurements: Flame arrival time, Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]Skjold, T. and Hisken, H. and Atanga, G. and Narasimhamurthy, V. D. and Lakshmipathy, S. and Storvik, I. E. and Pesch, L and Braatz, A. (2017), Final report 'JIP MEASURE'. Report number Gexcon-17-F46241-C-1
[2]D. Allason (2017), MEASURE Data Report. Report number 1Q14RQR-11 Rev. 2-0
[3]D. Allason (2017), MEASURE Data Analysis Report. Report number 1QI4RQR-19 Rev. 1-0
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL N MG VG FAC2 FB NMSE
PROPANE
oucrocro>。一」laJLUO① G
-0.34
0.14
• PROPANE
Geometric mean bias
Pressure
FUEL
MG
VG
FAC2 FB
NMSE
PROPANE
山 Duro_」p> u_」l ① EOOJO
0.68
• PROPANE
9.4
Geometric mean bias
10.3.2.20 MERGE
METHANE, PROPANE, ETHYLENE
The project MERGE (Modelling and Experimental Research into Gas Explosions) was undertaken to address key issues relating to the influence on over-pressure and flame acceleration from varying the volume blockage, pipe diameters and fuels for particular obstacle configurations. The experiments of MERGE involved a single array of pipes contained in a homogeneous gas cloud, enclosed in a
polythene tent [1]. The obstacles used were refered as type A [2], B [3], C [4], D [5], E [6] and CS [7].
Location: British Gas Fauld and Spadeadam test facilities (UK)
Year: 1991-1993
Number of cases in series: 19
Available measurements: Flame arrival time, Pressure
Grids used: 150 mm, 300 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Shale, A.G. & Walker, D.G. (1992), Modelling and Experimental Reseach into Gas Explosions (MERGE) - CEC Final Report.
[2]British Gas (BG) (1992), Results from experiments with obstacle type A. British Gas Research & Technology Report.
[3]British Gas (BG) (1992), Results from experiments with obstacle type B. British Gas Research & Technology Report.
[4]British Gas (BG) (1991), Results from experiments with obstacle type C. British Gas Research & Technology Report.
[5]British Gas (BG) (1992), Results from experiments with obstacle type D. British Gas Research & Technology Report.
[6]British Gas (BG) (1993), Results from experiments with obstacle type E. British Gas Research & Technology Report.
[7]British Gas (BG) (1993), Results from experiments with obstacle type CS. British Gas Research & Technology Report.
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL METHANE PROPANE
METHANE, PROPANE All fuels
N MG VG FAC2 FB NMSE
19 1 – 1.1 1 – 1.1 0.95 – 1 0.0028 – 0.028 0.0056 – 0.048
19 0.99 – 1.1 1 – 1.1 0.9 – 1 -0.1 – 0.043 0.014 – 0.057
18 0.86 – 0.93 1 – 1.2 0.89 – 1 -0.26 – -0.1 0.04 – 0.13
57 0.98 – 1 1 – 1.1 0.91 – 1 -0.12 – -0.013 0.021 – 0.081
• METHANE, PROPANE
• PROPANE
• METHANE
• ETHYLENE
IO-1 10° IO1
Geometric mean bias
0.2 0.4
Experiment [s]
Pressure
FUEL
METHANE
PROPANE
METHANE, PROPANE
ETHYLENE
N
15
19
20
10
MG
0.75 – 1.1
0.45 – 0.57
0.56 – 2.6
0.89
All fuels
54
0.59
gcoqj uoqcnlu-s
VG
1.1
2.1 – 2.9
1.6 – 3.9
1
FAC2
0.93 – 0.95
0.38 – 0.53
0.5 – 0.75
1
FB
-0.39 – -0.075
-1.1 – -0.91
-0.81 – 1
-0.12
NMSE
0.044 – 0.32
1.9 – 5
2.1 – 2.7
0.018
IO-1
• ETHYLENE
• METHANE, PROPANE
• PROPANE
• METHANE
1.8 – 4.3
Geometric mean bias
Experiment [barg]
10.3.2.21 Mogeleg Branches
PROPANE
Available measurements: Pressure
MOGELEG BRANCHES
Location:
Year:
Number of cases in series: 6
REFERENCES
The campiagn consists of series of gas explosion experiments conducted in a channel 1.5m*0.3m*0.3m to study the effect of vegetation in flame propagation. The effect of vegetation both in terms of tree species, number of branches and foliage presence is investigated. The propaneair mixture was filled in the channel with ignition source at centre of the closed end. Four pressure transucers were used with one fitted at clsed end while other three placed along the rear wall.[1]
SELECTION OF TESTS
SIMULATION SETUP
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①oup-」p> OCSEO^O
Geometric mean bias
.3
2
0.35 0.66 0.54
.5.4.32 「 0.0.0.0. "E^o-- Co^ra-DE-^
Experiment [barg]
10.3.2.22 MOGELEG Channel
MOGELEG CHANNEL
HYDROGEN, N2
A series of 56 tests were performed in a 0.13m3 test chamber at the Gexcon test laboratory at Fantoft, near Bergen, Norway. The vessel is rectangular in shape and is 1.44m long, 0.3m high and 0.3m wide. The test vessel contained baffle plate obstructions for turbulence generation. The vessel is closed on all sides and at one end. The fuel mixtures were usually ignited near the centre of the closed end of the chamber. All explosion venting occurred at the end of the vessel furthest from ignition. A limited number of tests were performed however, in which the ignition source was mounted at the upstream face of one of the baffle obstructions. The internal geometry of the vessel could be varied by the insertion of baffle plate obstructions of 5cm, which were fixed to the walls and floor of the vessel. Due to the high reactivity of the gas mixtures to be used, and to maintain integrity of the test chamber, 2 obstacle configurations (2 baffles and 4 baffles) were used in the current experiments in addition to tests performed in the empty chamber without obstructions. 4 gases were used in the tests (H2, 3H2+CO, H2+CO, 3H2+N2) at different concentrations in air [1].
Location: Gexcon AS, Bergen, Norway
Year: 2001-2002
Number of cases in series: 33
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
REFERENCES
FUEL
HYDROGEN HYDROGEN, N2
Pressure
N
108
24
132
MG 0.74 0.83
0.75
VG
2
1.1
FAC2 0.68 0.92
FB
0.13
-0.11
0.086
NMSE
3.1 0.072
2.5
①UUP_」Q> U-.P山EO山0
o2
1
1
1
All fuels
Geometric mean bias
15-
o
1
1.8
0.72
• HYDROGEN, N2
• HYDROGEN
5 10 15
Experiment [barg]
10.3.2.23 Molkov
PROPANE
The campaign consists of thirteen gas explosion tests conducted in cylindrical vessel of diameter 2m and length 3.5m. The vessel had a rectangular hole 1.7m high and 0.8m wide covered with sturdy paper at one of the edges. Propaneair mixture was used as fuel which was ignited by a point source located at 0.4m from covered edge on vessel axis. Obstacles were arranged in arrays in diametral plane of vessel. The internal pressure was measured by two pressure transducers. [1]
Location:
Year:
Number of cases in series: 14
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]V. V. Mol'kov and V. V. Agafonov and S. V. Aleksandrov (1997), Deflagration in a vented vessel with internal obstacles, Combustion, Explosion and Shock Waves
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①oup-」p> OCSEO^O
.5.0.5 1 1 o 【peq】 UOAru-nlu-s
0.86 0.56 0.44
• PROPANE
Geometric mean bias
Experiment [barg]
10.3.2.24 Park: Vented rectangular chamber
METHANE
Campaign consists of series of explosion test conducted inside rectangular chambers with 700mm x 700mm crosssection and a large top-venting area of 700mm x 210mm. The height of chamber was varied from 200mm to 1000mm. Three different multiple obstacles with square, circular and triangular cross-sections were used with diameters/size 70mm and 100mm respectively. Methane-air mixture in all tests was ignited near the bottom wall. Pressure values were recorded with transducer mounted on top wall of chamber, 20mm from exit.
Location:
Year:
Number of cases in series: 20
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 13 mm, 25 mm, 33 mm
REFERENCES
[1]Park, Dal and Lee, Y.s and Green, Anthony (2008), Experiments on the effects of multiple obstacles in vented explosion chambers,
Journal of hazardous materials
Pressure
FUEL N MG VG FAC2 FB NMSE
0 – 1 -1.1 – 0.77 0.11 – 1.7
METHANE 4 0.31 – 2.1
①OUP_」B> OC^OEO^O
lO1^
• METHANE
10.3.2.25 Shell 30m3 Harrison
ETHANE, METHANE, PROPANE
A series of vented explosion tests has been carried out using 30m3 explosion chamber.One end of the chamber was provided with square orifice, a series of area reducing plates with vent area 1/2,1/4 and 1/8 of area of end face were used.
Fuel used are propane and natural gas ignited within the chamber at different ignition location i.e centre, front and end of the chamber.[1].
Location:
Year:
Number of cases in series: 16
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 140 mm
REFERENCES
[1]A. J. HARRISON and J. A. EYRE (1987), External Explosionsa€^ as a Result of Explosion Venting, Combustion Science and Technology
FUEL
ETHANE, METHANE
PROPANE
Pressure
VG
1.7
1.5
FAC2 0.58 0.69
FB
-0.48
-0.47
NMSE 0.84 0.53
① UUP_」Q>uc」山 LUO 山 D
【&JBql uoqp-nE-s
• PROPANE
• ETHANE, METHANE
0.5 1.0 1.5
Experiment [barg]
10.3.2.26 Shell Hydrogen Repeated Pipe Congestion
HYDROGEN
Hydrogen-air mixtures were ignited in a 3 m x 3 m x 2 m congested area at the Health and Safety Laboratory [1]. Three different levels of congestion were used by varying the amount of repeated pipes in the rig. Both rich and lean hydrogen mixtures were used.
Location: UK, Health and Safety Laboratory
Year: 2006
Number of cases in series: 7
SELECTION OF TESTS
Available measurements: Flame arrival time, Pressure
SIMULATION SETUP
Grids used: 133 mm
REFERENCES
[1]Shirvill, L.C. & Roberts, T.A & Royle, M. & Willoughby, D.B & Sathiah, P. (2019), Experimental study of hydrogen explosion in repeated pipe congestion Part 1: Effects of increase in congestion, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL N MG VG FAC2 FB NMSE
①OUP_」B> OC^OEOau
1.8 1.7
6 4 2 .O.O.O o.o.o. 〔s】uo_】-nE_s
0.64 0.52
0.00
0.00 0.02 0.04 0.06
Experiment [s]
0.36
• HYDROGEN
Pressure
FUEL
N MG VG
FAC2
FB
NMSE
IO"1
10°
2 2 11 【praq】 UOQ-nLU-s
0.16
• HYDROGEN
Geometric mean bias
Experiment [barg]
10.3.2.27 Shell NaturalHy Repeated Pipe Congestion
HYDROGEN, METHANE
Hydrogen-air mixtures were ignited in a 3 m x 3 m x 2 m congested area at the Health and Safety Laboratory [1]. The congested area consisted of repeated pipes. The amount of hydrogen in the experiments was varied from 0 (100\% methane) to 100 (0\% methane)..
Location: UK, Health and Safety Laboratory
Year: 2006
Number of cases in series: 5
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 133 mm
REFERENCES
[1]Shirvill, L.C., Roberts, T.A., Royle, M,. Willoughby, D.B, Sathiah, P. (2019), Experimental study of hydrogen explosion in repeated pipe congestion Part 2: Effects of increase in hydrogen concentration in hydrogen-methane-air mixture, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
Geometric mean bias
Experiment [barg]
• HYDROGEN, METHANE
• METHANE
• HYDROGEN
• Deflagration X Detonation
10.3.2.28 Solvex
SOLVEX
METHANE, PROPANE
The campaign consisted of gas explosions in large scale enclosure with size 10m*8.75m*6.25m and vent located at centre of the front wall. The experiments were performed with propane-air and methane-air mixtures iside the enclosure ignited by a point ignition source located at centre of the rear wall. The tests were conducted with empty encloure configuration, one or two rows of 0.5m diameter pipes.[1][2]
Location: Shell UK
Year:
Number of cases in series: 8
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 386 mm
REFERENCES
[1]Molkov, Vladimir and Makarov, Dmitriy and Puttock, Jonathan (2006), The nature and large eddy simulation of coherent deflagrations in a vented enclosure-atmosphere system, Journal of Loss Prevention in The Process Industries - J LOSS PREVENT PROC IND
[2]Vianna, Savio and Cant, R. (2010), Modified porosity approach and laminar flamelet modelling for advanced simulation of accidental explosions, Journal of Loss Prevention in the Process Industries
FUEL
METHANE, PROPANE
PROPANE
Pressure
N MG VG
4 2.1 1.9
FAC2
0.5
0.75
FB
0.83
0.68
NMSE
1.4
0.83
①:>UQ_」P> UC^EO^m^
.8.6.42
0.0.
巨鼻 UOQP-nE-s
Geometric mean bias
• PROPANE
• METHANE, PROPANE
10.3.2.29 SRI Confined Tube
HYDROGEN
The facility consists of a square section steel tube with an inside dimension of 38.1 cm and a length of 990 cm. The ignition end of the tube was closed with a steel plate and the opposite end was opened prior to ignition by piercing a latex rubber diaphragm stretched tightly over the end. Various obstacle configurations were used to promote turbulence of the flame propagation. Figure 1 is a cross section of the tube showing the layout of the obstacles. The steel obstacles were 6.35 cm thick and were attached to a steel floor that was 1.27 cm thick on top of 1.91-cm-thick risers. Blockage ratios of 0.32, 0.47, and 0.65 were obtained using blocks that had heights of 11.43 cm, 16.51 cm, and 22.86 cm. The blocks were spaced at regular intervals of 38.1 cm, 76.2 cm, or 152.4 cm for tests using 25 blocks, 13 blocks, or 7 blocks respectively. The first block was always 38.1 cm from the initiation end.
Location: DoE, USA
Year: 2002
Number of cases in series: 8
SELECTION OF TESTS
Available measurements: Flame arrival time, Pressure
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame arrival time
FUEL N MG VG FAC2 FB NMSE
0.88
①:}up_」e> D-JIBIUOBD
HYDROGEN
146
〔2 uoqp-nlu-s
0.06
0.05
0.04
0.03
0.02-
ld-1......io° ......io1
Geometric mean bias
1.1 0.92 -0.16 0.11
• HYDROGEN
• Detonation X Deflagration
0.014-------.------------,------------
0.02 0.04 0.06
Experiment [s]
Pressure
FUEL
N MG
VG FAC2
FB
NMSE
1
• HYDROGEN
• Detonation
X Deflagration
IO-1
10°
Geometric mean bias
10 20 30
Experiment [barg]
10.3.2.30 TNO 39m3
METHANE
The experiments were conducted in a concrete enclosure of size 4mx3.7mx2.6m with an internal volume of 38.5m3. Methane-air mixture was filled in the enclosure through three locations. Ignition source varied across the campaign with locations at rear, centre and near vent. Three pressure transducers were mounted inside the enclosure. Different vent configurations were used with single or multiple layers of polyethylene sheet and single plaster sheet plate as vent cover. Few tests were conducted with a single large obstacle placed at centre of the enclosure.[1]
Location:
Year:
Number of cases in series: 6
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 173 mm
REFERENCES
[1]W.P.M. Mercx, C.J.M. van Wingerden, H.J. Pasman (1992), Venting of Gaseous Explosions
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
①OUP_」B> OC^OEO^O
〔praq〕uo-lp-nuj-s
Geometric mean bias
4.1e+02 0 -1.7
11
0.20
0.15
0.10
0.05
• METHANE
0」 0:2
Experiment [barg]
10.3.2.31 Traffic Tunnel Square
TRAFFIC TUNNEL SQUARE
HYDROGEN
Hydrogen explosion in a traffic tunnel (with and without cars). The experimental set-up consisted of a 78.5m long tunnel with a diameter of 2.4 m and a cross-sectional area of
3.74 m2. The experimental facility was a one-fifth scale mock-up of a typical tunnel for road transport. The explosive hydrogen-air mixture was located in a 10 m long region, filling a volume equal to 37 m3. Several experiments were carried out, using different hydrogen concentration. The experiments with 30% hydrogen volumetric concentration in air have been considered. The geometry set-up was either an empty tunnel or a tunnel with 4 vehicle models on the floor
centreline inside the hydrogen-air mixture. The vehicle models measured 0.94 m in length, 0.362 m in width and 0.343 m in height, representing typical real-vehicles at onefifth scale. The distance between vehicles was 1.52 m. The blockage ratio due to the presence of the vehicles was 0.03. Pressure transducers were mounted on the side wall of the
tunnel along its entire length. The ignition position was located in the middle of the tunnel for all experiments.
Location:
Year: 2009
Number of cases in series: 2
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
REFERENCES
[1]Middha, P. & Kotchourko, A. (2010), CFD calculations of gas leak dispersion and subsequent gas explosions: Validation against ignited impinging hydrogen jet experiments, Journal of Hazardous Materials
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
QUG^Cro> u-」4-1山 LU 090
0.81
8 6 4 2 0 11111 【PQq】 UOA-nE-s
1 1 -0.21 0.047
• HYDROGEN
Geometric mean bias
Experiment [barg]
Case name Type Variable Metrics
N MG VG FAC2 FB NMSE
|
Dispersion |
Fuel volume fraction |
14 |
0.24 |
5.8e+05 |
0.64 |
-0.39 |
1.4 | |
|
CHRC |
Dispersion |
Fuel volume fraction |
16 |
0.4 |
2.6 |
0.25 |
-1 |
43 |
|
Coyote |
Dispersion |
Fuel volume fraction |
15 |
0.093 |
2.6e+19 |
0.73 |
-0.14 |
0.19 |
|
HySEA INHOMOGENEOUS RELEASE |
Dispersion |
Fuel volume fraction |
48 |
1.1-1.5 |
1-1.2 |
0.94-0.98 |
0.075-0.38 |
0.022-0.15 |
|
KitFox |
Dispersion |
Fuel volume fraction |
153 |
1.1 |
1.6 |
0.73 |
0.03 |
0.62 |
|
Maplin Sands |
Dispersion |
Fuel volume fraction |
10 |
0.98 |
1.1 |
0.9 |
-0.14 |
0.059 |
|
Warehouse sandia release |
Dispersion |
Fuel volume fraction |
6 |
1.1 |
1.1 |
0.83 |
0.14 |
0.057 |
|
Thorney island |
Dispersion |
Fuel volume fraction |
15 |
0.98 |
1.6 |
0.67 |
-0.032 |
0.21 |
|
LLNL Falcon |
Dispersion |
Fuel volume fraction |
3 |
0.32 |
5 |
0.33 |
-1.2 |
3 |
Table 10.2: Dispersion validation cases.
10.3.3 Dispersion
Figure 10.3 (top-centre) summarises the presented dispersion validation cases in a single scatter plot, while table 10.2 gives a summary of the individual experiments. Performance is very good across the different fuel types and ambient conditions. In general, the outliers can be explained by challenges modelling the variation of wind speed and direction in large-scale dispersion experiments. Measurements in experiments are typically across an arc-wise array of sensors. Narrow plumes sometimes miss all of the sensors on an arc, the resulting low concentration at the corresponding arc-distance causes problems in calculating the geometric mean and variance.
10.3.3.1 Burro Tests
|
BURRO | |
|
METHANE The Burro field experiments consisted of nine large spills of LNG onto a 1-m-deep pool of water [1][2][3][4][5][6]. The four selected test cases are those which have been most extensively analysed and cover the widest wide range of meteorological and spill conditions. | |
|
Location: China Lake testing site, California, U.S. Year: 1980 Number of cases in series: 4 | |
|
SELECTION |
OF TESTS |
|
Available measurements: Fuel volume fraction | |
|
SIMULATI |
ON SETUP |
|
Grids used: 625 mm |
■a y |
|
REFER |
ENCES |
|
[1]Ermak, D. L., Chapman, R., Goldwire, H. C. Jr., Gouveia, F. J. & Rodean Lawrence Livermore National Laboratory., Lawrence Livermore Natio [2]Koopman, R. P., Cederwall, R. T., Ermak, D. L., Goldwire, Jr H. C., Hog Shinn, J. H. (1982), Analysis of Burro series 40 m3 LNG spill experime [3]Koopman, R. P., Baker, J., Cederwall, R. T., Goldwire, H. C. Jr, Hogan, Morgan, D. L., Morris, L. K., Spann, M. W. Jr & Lind, C. D. (1982), LLNL/ LNG spill tests. Burro series data repor.. Report number UCID-19075-V [4]Ivings M.J., Gant S.E., Jagger S.F., Lea C.J., Stewart J.R. and Webber LNG facilities., Health & Safety Laboratory [5]Mauri, L. (2016), Evaluation of FLACS Performance Against the Mod F46033-C-1 [6]Stewart, J.R., Coldrick, S., Lea, C.J., Gant, S.E. & Ivings, M.J. (2016), G |
, H. C. (1988), Heavy gas dispersion test summary report. s.l.: nal Laboratory. Report number ADA213880 an, W. J., McClure, J. W., McRae, T. G., Morgan, D. L., Rodean, H. C. & nts, Journal of Hazardous Materials W. J., Kamppinen, L. M., Kiefer, R. D., McClure, J. W,, McCrae, T. G., WC 1980 LNG spill tests. Burro series data reportLLNL/NWC 1980 ol.1 ON: DE84000921 D.M. (2016), Evaluating vapor dispersion models for safety analysis of el Validation Database, appendix 1. Report number GexCon-14- uide to the LNG model validation database version 12. |
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
^uc^cra> u--GJUJO① o
7.1e+02 0.64 -0.39
60
40
20
0
1.4
Geometric mean bias
• METHANE
0 20 40 60
Experiment [vol%]
10.3.3.2 CHRC
CO2, PROPANE
CHRC carried out wind-tunnel experiments on the dispersion of carbon dioxide (CO2), both with and without obstacles [1]
[2] . One of the aims of the experiments was to produce validation data for the FEM3A dispersion model [3].The wind tunnel was an ultra-low-speed boundary-layer wind tunnel capable of simulating the constant stress layer of the atmospheric boundary layer. Airflow from the driving fans passed through a circular-to-rectangular transition to a 7 ft. high, 20 ft. wide and 80 ft. long working area in which the floor was covered with smooth rubber matting on which roughness elements were mounted.The obstacles, dike was square with an inner dimension of 63 cm and a wall height of 3.7 cm and the model tank was 31 cm in diameter with a hemi-spherical dome top and an overall height of 28.3 cm
Location: University of Arkansas, USA,
Year: 1988
Number of cases in series: 3
SELECTION OF TESTS
Available measurements: Fuel volume fraction
SIMULATION SETUP
Grids used: 6 mm
REFERENCES
[2]Stewart, Jim and Coldrick, Simon and Lea, Chris and Gant, Simon and Ivings, Mat (2016), Validation Database for Evaluating Vapor
Dispersion Models for Safety Analysis of LNG Facilities: Guide to the LNG Model Validation Database Version 12
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
o o o
3 2 1 【%o>uo 一J-JBl-s
①uup_」e> U-GJUJO ① o
Geometric mean bias
10.3.3.3 Coyote Tests
|
COYOTE | |
|
METHANE The Coyote field experiments consisted of ten large spills of LNG onto a 1-m-deep pool of water. The three selected test cases are those which have been most extensively analyzed and are regarded as benchmarks for dispersion model validation [1][2][3][4][5]. | |
|
Location: China Lake testing site, California, U.S. Year: 1981 Number of cases in series: 3 | |
|
SEL |
ECTION OF TESTS |
|
Available measurements: Fuel volume fraction | |
|
SIM |
ULATION SETUP |
|
Grids used: 40 mm |
,: 一^^ |
|
REFERENCES | |
|
[1]Ermak, D. L., Chapman, R., Goldwire, H. C. Jr., Gouveia, F. J. & Lawrence Livermore National Laboratory., Lawrence Livermor [2]Goldwire, H. C. Jr, Rodean, H. C., Cederwall, R. T., Kansa, E. J. Kiefer, R. D. (1983), Coyote series data report: LLNL/NWC 1981 L and 2., Lawrence Livermore National Laboratory. Report numb [3]Ivings M.J., Gant S.E., Jagger S.F., Lea C.J., Stewart J.R. and LNG facilities., Health & Safety Laboratory [4]Mauri, L. (2016), Evaluation of FLACS Performance Against t F46033-C-1 [5]Stewart, J.R., Coldrick, S., Lea, C.J., Gant, S.E. & Ivings, M.J. ( |
Rodean, H. C. (1988), Heavy gas dispersion test summary report. s.l.: e National Laboratory. Report number ADA213880 , Koopman, R. P., McClure, J. W., McCrae, T. G., Morris, L. K., Kamppinen, L., NG spill tests dispersion, vapor burn and rapid-phase transitions. Volumes 1 er UCID-19953 ebber D.M. (2016), Evaluating vapor dispersion models for safety analysis of he Model Validation Database, appendix 1. Report number GexCon-14- 2016), Guide to the LNG model validation database version 12. |
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL
MG
VG
FAC2 FB
NMSE
METHANE
15
0.093
IO-1
10°
2.6e+19 0.73 -0.14 0.19
Geometric mean bias
Experiment [vol%]
10.3.3.4 HySEA Inhomogeneous Release
HYDROGEN
66 vented hydrogen deflagration experiments were performed in a 20-foot ISO containers. 22 tests were performed involving either an empty container with only the frame inserted, or a pipe rack installed in centre position inside the container. The experiments involved release of hydrogen inside the container either from a circular pipe or from a cubical box located at floor centre of the container and above floor and later ignited with ignition location on the upper back wall [1][2].
Location: Gexcon AS (Norway)
Year: 2016-2018
Number of cases in series: 12
SELECTION OF TESTS
Available measurements: Fuel volume fraction
SIMULATION SETUP
Grids used: 100 mm, 150 mm
REFERENCES
[1]Lucas, M, Skjold, T. & Hisken, H. (2020), Computational fluid dynamics simulations of hydrogen releases and vented deflagrations in large enclosures., Journal of Loss Prevention in the Process Industries
[2]Skjold, T., Hisken, H., Lakshmipathy, S., Atanga, G., van Wingerden, M., Olsen, K. L., Holme, M. N., Turøy, N. M., Mykleby, M., van Wingerden, K. (2019), Vented hydrogen deflagrations in containers Effect of congestion for homogeneous and inhomogeneous mixtures., International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
①uup_」e> UC^OEOa^
1.2 0.94 – 0.98
0.022 – 0.15
Geometric mean bias
%0>u04B-nLU 一 s
40
30
20
10
0.075 – 0.38
20 40
Experiment [vol%]
• HYDROGEN • 100 mm X 150 mm
10.3.3.5 LLNL Falcon Tests
LLNL FALCON
METHANE
The Falcon tests [1] were performed to verify the effectiveness of vapour barriers in reducing the risk associated with the release and dispersion of LNG.The spill was distributed over the water pond by a 4-arms piping system. The spill pond was surrounded by a high fiberglass fence and upwind of the spill pond a @€xbillboard@€M structure was mounted to reproduce the typical turbulence generated by a storage tank.The three Falcon test cases are those which are regarded as benchmarks [2]. [3], [4][5]
Location: Franchman Flat (Nevada),U.S
Year: 1987
Number of cases in series: 3
SELECTION OF TESTS
Available measurements: Fuel volume fraction
SIMULATION SETUP
REFERENCES
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
3
• METHANE
o o o o 4 3 2 1 【%o>uo 一J-JB1 一 S
10° 101
--.
2
1
10°-10-1
Geometric mean bias
^uc^cra> u--GJUJO① o
10.3.3.6 Kit Fox
CO2
Dense gas carbon dioxide (CO2) was released at ground level for longer time periods (continuous "plumes") and for shorter time (short-duration transient "puffs"), including both neutral and stable conditions. The desert surface, a dry lake bed known as Frenchman Flat, was artificially roughened using combinations of flat billboard obstacles in order to simulate the roughness of an industrial site and its surroundings at about 1/10 scale. The roughness elements were constructed from a plywood billboards and were catergorised as Equivalent Roughness Pattern (ERP, 2.4m x 2.4m) and Uniform Roughness Array (URA, 0.2m high x 0.8m wide). The roughness elements were installed along the cross-wind (y direction) and along-wind (x direction). O2 was released from a 1.5m x 1.5m area source, with a nearly constant emission rate. 84 concentration monitors were installed on the four downwind arcs (25, 50, 100, and 225m).
Meteorological instruments were installed on five towers with heights 24m (EPA), 4.9m (Met1), 8m (Met2), 4.9m (Met3), and 8m (Met4). Puff releases experiments comprised of 34, finite duration (20 seconds) tests. 13 tests were performed with URA and ERP in place, while 21 test with ERP removed [1]
Location: Frenchman Flat, Nevada, U.S.A.
Year: 1995
Number of cases in series: 51
SELECTION OF TESTS
Available measurements: Fuel volume fraction
SIMULATION SETUP
Grids used: 120 mm
REFERENCES
[1]Hanna, S.R & Chang, J.C (2001), Use of the Kit Fox field data to analyze dense gas dispersion modeling issues, Atmospheric Environment
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL
MG
VG
FAC2
FB
NMSE
153
2 1
o o
1 1
①oUB_」e> UC^OEOao
10。三 IO-1
10°
2 4 6
Geometric mean bias
Experiment [vol%]
10.3.3.7 Maplin Sands
|
MAPLIN SANDS | |
|
METHANE The Maplin Sands trials were conducted by Shell Research Limited in 1980 and consisted of 34 spills of liquefied gases onto the sea. Both continuous and instantaneous releases of LNG and LPG were carried out through a vertical pipe terminating above the water surface. The release site was an area of tidal sands in the Thames estuary so that the cloud dispersion occurred over flat terrain [1][2][3] [4][5]. The selected Maplin Sands test cases are three of the four releases in the Modelers Data Archive. Case 29 is omitted, since Ermak et al. [6] stated that for this case sub-surface vaporization was considerable, leading to gas jetting as high as 10 m in the source area, such that specification of a vapor source term could prove problematic. | |
|
Location: Maplin Sands (Thames estuary), U.K. Year: 1980 Number of cases in series: 3 | |
|
SELECTION |
OF TESTS |
|
Available measurements: Fuel volume fraction | |
|
SIMULATI |
ON SETUP |
|
Grids used: 50 mm | |
|
REFER |
ENCES |
|
[1]Ermak, D. L., Chapman, R., Goldwire, H. C. Jr., Gouveia, F. J. & Rodean Lawrence Livermore National Laboratory., Lawrence Livermore Natio [2]Puttock, J. S., Blackmore, D. R. & Colebrander, G. W. (1982), Field exp [3]Ivings M.J., Gant S.E., Jagger S.F., Lea C.J., Stewart J.R. and Webber LNG facilities., Health & Safety Laboratory [4]Mauri, L. (2016), Evaluation of FLACS Performance Against the Mod F46033-C-1 [5]Stewart, J.R., Coldrick, S., Lea, C.J., Gant, S.E. & Ivings, M.J. (2016), G [6]Ermak, D. L., Chapman, R., Goldwire, H. C. Jr., Gouveia, F. J. & Rodean Lawrence Livermore National Laboratory., Lawrence Livermore Natio |
, H. C. (1988), Heavy gas dispersion test summary report. s.l.: nal Laboratory. Report number ADA213880 eriments on dense gas dispersion., Journal of Hazardous Materials D.M. (2016), Evaluating vapor dispersion models for safety analysis of el Validation Database, appendix 1. Report number GexCon-14- uide to the LNG model validation database version 12. , H. C. (1988), Heavy gas dispersion test summary report. s.l.: nal Laboratory. Report number ADA213880 |
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
1.1
12.5
10.0-
.5.0.5
7.5.2.
【%-0>u0_-l->6nE 一 s
①OUP_」B> OC^OEO^O
Geometric mean bias
10.3.3.8 Thorney Island
BUTANE, PROPANE
In the Thorney Island continuous release experiments, a mixture of 32% R-12 and 68% nitrogen was released through a duct emerging from the ground and capped by 2 m diameter plate. The resulting outflow had zero vertical momentum and low radial momentum flow, comparable to a gravity current velocity [1][2][3][4][5]. Among the three trials, test number 46 was excluded because of the limited data due to changes in the wind direction during the experiment.
Location: Thorney Island, U.K.
Year: June 15,1984
Number of cases in series: 2
SELECTION OF TESTS
Available measurements: Fuel volume fraction
SIMULATION SETUP
Grids used: 380 mm
REFERENCES
[1]Ermak, D. L., Chapman, R., Goldwire, H. C. Jr., Gouveia, F. J. & Rodean, H. C. (1988), Heavy gas dispersion test summary report. s.l.:
Lawrence Livermore National Laboratory., Lawrence Livermore National Laboratory. Report number ADA213880
[2]Ivings M.J., Gant S.E., Jagger S.F., Lea C.J., Stewart J.R. and Webber D.M. (2016), Evaluating vapor dispersion models for safety analysis of
LNG facilities., Health & Safety Laboratory
[3]Mauri, L. (2016), Evaluation of FLACS Performance Against the Model Validation Database, appendix 1. Report number GexCon-14-
F46033-C-1
[4]McQuaid, J. & Roebuck, B. (1985), Large-Scale Field Trials on Dense Vapour Dispersion
[5]Stewart, J.R., Coldrick, S., Lea, C.J., Gant, S.E. & Ivings, M.J. (2016), Guide to the LNG model validation database version 12.
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
^ucrocra> :HJJOJEO ①o
15
【%-0>u0-l—lB-nE_s
2
-0.032 0.21
0.98 1.6 0.67
• BUTANE, PROPANE
10 20
Geometric mean bias
Experiment [vol%]
10.3.3.9 Warehouse Sandia Release
HYDROGEN
The experiments were performed in a scaled model of a warehouse facility. The dimensions were 3.64 m wide by 4.59 m long by 2.72 m high, with a total volume of 45.4 m3. The mass of hydrogen was released into warehouse and the concentration variation with time was measured [1][2].
Location: Livermore, California Year: 2011
Number of cases in series: 1
Available measurements: Fuel volume fraction
Grids used: 26 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Ekoto, I.W., Merilo, E.G., Houf, W.G., Evans, G.H. & Groethe, M.A. (2012), Experimental investigation of hydrogen release and ignition from fuel cell powered forklifts in enclosed spaces., International Journal of Hydrogen Energy
[2]W.G. Houf and G.H. Evans and I.W. Ekoto and E.G. Merilo and M.A. Groethe (2013), Hydrogen fuel-cell forklift vehicle releases in enclosed spaces, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Fuel volume fraction
FUEL N MG VG FAC2 FB NMSE
^ucrocra> ULIJBEOBO
o o o o o 0 8 6 4 2 1
【%o>UOA-nlu 一 s
0.83 0.14 0.057
Geometric mean bias
Experiment [vol%]
|
Case name Type Variable Metrics N MG VG FAC2 FB NMSE | ||||||||
|
Gasoline 0p3m pool fire |
Fire |
Radiative Flux |
13 |
1.4 |
1.2 |
1 |
0.37 |
0.29 |
|
GL Hydrogen Jet Fire |
Flame length |
2 |
0.86 |
1 |
1 |
-0.17 |
0.041 | |
|
Flame trajectory |
70 |
1.3 |
1.2 |
0.8 |
0.38 |
0.41 | ||
|
Radiative Flux |
26 |
0.62 |
1.7 |
0.62 |
-0.39 |
1.2 | ||
|
HSL hydrogen impinging fire |
Fire |
Radiative Flux |
22 |
2.2 |
4.8 |
0.41 |
0.84 |
2.3 |
|
LNG Flare |
Fire |
Radiative Flux |
31 |
1.7 |
2.4 |
0.39 |
0.7 |
1.1 |
|
LNG FOAMGLAS |
Radiative Flux |
4 |
0.76 |
1.1 |
1 |
-0.28 |
0.094 | |
|
Montoir Pool Fire |
Fire |
Radiative Flux |
3 |
0.32 |
4.6 |
0.33 |
-1.2 |
4.6 |
|
Naturalhy Jet Fire |
Fire |
Flame length |
2 |
0.85-0.96 |
1 |
1 |
•0.16 - -0.041 |
0.0017-0.027 |
|
Flame trajectory |
69 |
0.92 - 1 |
1-1.1 |
0.97 -1 |
-0.19-0.0081 |
0.01-0.24 | ||
|
Radiative Flux |
24 |
0.81-1.1 |
1.1-1.3 |
0.83 -1 |
-0.21-0.27 |
0.1-0.5 | ||
|
Sandia Cryogenic Hydrogen Jet Fires |
Flame length |
5 |
1.1 |
1 |
1 |
0.11 |
0.013 | |
|
Radiative Flux |
25 |
1.7 |
1.5 |
0.68 |
0.6 |
0.59 | ||
|
SINTEF Impinging Jet |
Fire |
Radiative Flux |
6 |
0.54 |
1.6 |
0.67 |
•0.58 |
0.45 |
Table 10.3: Fire validation cases.
10.3.4 Fire
Figure 10.3 (top-right) summarises the presented fire validation cases in a single scatter plot, while table 10.3 gives a summary of the individual experiments.
The FLACS-CFD fire solver generally performs well for jet fires including horizontal and vertical jet fires, with or without crosswind, open, or impinging. Generally, parameters like flame length, flame trajectory, flame temperature, radiative and total heat flux compare well against experiments. Fire simulations for large horizontal non-impinging jet fires are shown to be dominated by significantly more buoyancy forces on the end part of the flame, causing the flame to bend off and rise up earlier compared to the experimental flame. The FLACS-CFD fire solver performs well for both steady flow rate and blowdown scenarios for various species including hydrogen.
10.3.4.1 Sandia Cryogenic Hydrogen Jet Fires
HYDROGEN
The experiments were conducted at the Turbulent Combustion Laboratory of SNL in USA. The main aim of the experiments was to investigate the ignition and flame characteristics of cryogenic underexpanded jet fires. The analysed scenarios were concerned with hydrogen releases with temperature in the range 37-295 K and pressure 2-6 bar abs. The release temperature and pressure were maintained constant during each test and monitored upstream the interchangeable orifice of diameter 0.75 mm or 1 mm or 1.25 mm. The hydrogen was released vertically upward in the laboratory equipped with an exhaust gas collection system. The incident thermal radiation was monitored at 5 sensors located along the jet flame and at 0.2 m from the jet axis. Five tests with orifice diameter 1.25mm out of the entire set of experiments performed by SNL have been selected for the validation [1][2][3].
Location: Sandia National Laboratories, USA
Year: 2015
Number of cases in series: 5
SELECTION OF TESTS
Available measurements: Flame length, Radiative Flux
SIMULATION SETUP
Grids used: 100 mm
REFERENCES
[1]Pratikash P. Panda and Ethan S. Hecht (2017), Ignition and flame characteristics of cryogenic hydrogen releases, International Journal of Hydrogen Energy
[2]D.M.C. Cirrone and D. Makarov and V. Molkov (2019), Thermal radiation from cryogenic hydrogen jet fires, International Journal of
Hydrogen Energy
[3]Muthusamy, D. (2019), Description of detailed scenarios for validation of consequence modelling tools - Gaseous hydrogen transport and use. Report number GEXCON-SH2IFT-WP3-2019-04_D3-2
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame length
FUEL N MG VG FAC2 FB NMSE
QUG^Cro> u-」4-1山 LU 090
【UJ】uo一jo-nE-s
0 9 8 7 6 Lo.0.0.0.
1 1 0.11 0.013
• HYDROGEN
Geometric mean bias
Experiment [m]
FUEL
N
Radiative Flux
MG VG
FAC2 FB
NMSE
0.59
• HYDROGEN
IO-1 10° IO1 2.5 5.0 7.5
Geometric mean bias Experiment [kW/m2]
10.3.4.2 GL Hydrogen Jet Fire
GL HYDROGEN JET FIRE
HYDROGEN
Two large-scale hydrogen jet fire experiments were conducted at the GL Noble Denton Spadeadam Test Site in North Cumbria, UK. Compressed hydrogen gas was released from a nominal 60 bar stagnation pressure through a horizontally orientated 1 m long stretch of pipe with respective internal diameters of 20.9 and 52.5 mm and located 3.25 m above the ground. Wind speed for test with smaller diameter nozzle was measured as 2.84m/s at 68.5deg from true north while for the other case wind speed was 0.83m/s at 34deg from true north. Incident thermal radiation was measured at 13 locations by wide-angle Medtherm radiometers mounted on tripods around the test area [1][2].
Location: GL Noble Denton Spadeadam Test Site, North Cumbria, UK
Year: 2008
Number of cases in series: 2
SELECTION OF TESTS
Available measurements: Flame length, Flame trajectory, Radiative Flux
SIMULATION SETUP
Grids used: 4000 mm
REFERENCES
[1]Ekoto, I.W, Houf, W.G., Ruggles, A.J., Creitz, L.W, Li, J.X. (2013), Large-scale hydrogen jet flame radiant fraction measurements and modeling
[2]I.W. Ekoto and A.J. Ruggles and L.W. Creitz and J.X. Li (2014), Updated jet flame radiation modeling with buoyancy corrections, International Journal of Hydrogen Energy
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame length
FUEL N MG VG FAC2 FB NMSE
①uup_」e> UC^OEOa^
6 .8
Geometric mean bias
o o o o 5 4 3 2 【Lu〕UOA-nuJ-s
Radiative Flux
FUEL
N MG
VG
FAC2
FB
NMSE
.62
HYDROGEN
26
IO"1
10°
o o o
6 4 2 ne/mxi u04qnE_s
Experiment [kW/m2]
Geometric mean bias
10.3.4.3 HSL Hydrogen Impinging Fire
HYDROGEN
A series of jet fire tests was performed to investigate the effectiveness of barrier walls at preventing radiation and physical transport of fire from hydrogen jet flames. Comparison of the reduction of jet-fire hazard by using 90deg and 60deg inclined walls to a free jet was done in terms of both thermal radiation and overpressures. Hydrogen was released at 200 barg through a nozzle of either 9.5, 6.4 or 3.2 mm.
Location: Health and Safety Laboratory (UK)
Year: 2009
Number of cases in series: 6
SELECTION OF TESTS
Available measurements: Radiative Flux
SIMULATION SETUP
Grids used: 3 mm
REFERENCES
[1]D.B. Willoughby and M. Royle (2011), The interaction of hydrogen jet releases with walls and barriers, International Journal of Hydrogen Energy
DATE: FEBRUAR 16, 2023 POSTPROCESS QUANTITIES
Radiative Flux
FUEL N MG VG FAC2 FB NMSE
山OUP-」Q> D-JIBEOBO
o2 1
1
1
0°
1
Geometric mean bias
.8
4 o o o o o I o o o o o 5 4 3 2 1 2.2 -^EB- UOA-nlu 一 s 2
200 400
Experiment [kW/m2]
• HYDROGEN
.3
2
10.3.4.4 LNG Flare
METHANE
Large-scale turbulent natural gas/air diffusion flames were used to evaluate analysis of flame structure and radiation properties. Radiation from turbulent diffusion flames dominates energy transport from unwanted fires, influencing their burning and growth rates. The experiments involved vertically upward injection of natural gas (96% methane by volume) in still air. Seven flames were tested (flame heights apporx. 25 m) with chemical energy release rates in the range of 135-210MW.
Location: USA
Year: 1986
Number of cases in series: 7
SELECTION OF TESTS
Available measurements: Radiative Flux
SIMULATION SETUP
Grids used: 250 mm
REFERENCES
[1]J. Gore and G. Faeth and D. Evans and Db Pfenning (1986), Structure and Radiation Properties of Large-scale Natural Gas/Air Diffusion Flames, Fire and Materials
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Radiative Flux
FUEL N MG VG FAC2 FB NMSE
^uc^cra> u--GJUJO① o
7
1.
Geometric mean bias
Experiment [kW/m2]
10.3.4.5 Naturalhy Jet Fire
ETHANE, HYDROGEN, METHANE, N2
A series of six large scale high pressure, jet fires experiments were conducted using natural gas and natural gas-hydrogen (approximately 24% by volume) mixtures. For each fuel, the three tests involved horizontal releases from 20, 35 and 50mm diameter holes at a gauge pressure of approximately 60 bar. The fires also engulfed a 1m diameter horizontal pipe placed across the flow direction and about halfway along the flame. This pipe was instrumented to measure the heat fluxes to the pipe.
Location: GL Noble Denton Spadeadam Test Site, North Cumbria, UK
Year: 2005
Number of cases in series: 6
SELECTION OF TESTS
Available measurements: Flame length, Flame trajectory, Radiative Flux
SIMULATION SETUP
Grids used: 100 mm, 180 mm, 190 mm, 260 mm
REFERENCES
[1]Barbara Joan Lowesmith and Geoffrey Hankinson (2012), Large scale high pressure jet fires involving natural gas and natural gas/hydrogen mixtures, Process Safety and Environmental Protection
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Flame length
FUEL
ETHANE, HYDROGEN, METHANE, N2
ETHANE, METHANE, N2
^u^^^ocqOJLUO①。
N MG VG FAC2
1 0.87 – 0.99 1 1
1 0.83 – 0.92 1 1
– 0.96
50-
o o o 4 3 2 UOA3nLU-s
Geometric mean bias
FB
-0.14 – -0.0092
-0.18 – -0.086
NMSE
8.5e-05 – 0.019
0.0074 – 0.033
0.0017 – 0.027
-0.16 – -0.041
Experiment [m]
ETHANE, METHANE, N2
ETHANE, HYDROGEN, METHANE, N2
190 mm
100 mm
260 mm
180 mm
Radiative Flux
|
FUEL |
N |
MG |
VG |
FAC2 |
FB |
NMSE |
|
ETHANE, HYDROGEN, METHANE, N2 |
12 |
0.81 – 0.96 |
1.1 – 1.4 |
0.75 – 1 |
-0.22 – -0.036 |
0.1 – 0.26 |
|
ETHANE, METHANE, N2 |
12 |
0.81 – 1.4 |
1.1 – 1.3 |
0.83 – 1 |
-0.21 – 0.31 |
0.11 – 0.5 |
|
All fuels |
12 |
0.81 – 1.1 |
1.1 – 1.3 |
0.83 – 1 |
-0.21 – 0.27 |
0.1 – 0.5 |
ETHANE, METHANE, N2
ETHANE, HYDROGEN, METHANE, N2
mm mm mm mm
10.3.4.6 LNG Foamglas Pool Fire
METHANE
The release of flammable gases, such as Liquefied Natural Gas (LNG) or Liquefied Petroleum Gas (LPG), may result in the formation of a flammable vapour cloud that is often dense, depending on the ambient conditions (particularly wind speed and direction). If this cloud encounters a source of ignition within the surrounding environment, a fire may occur. The characteristics of the resulting fire are dependent upon the release conditions and the environment into which the vapours are released. One test was conducted and the results of the test featuring the use of the passive material (FOAMGLAS® PFS System (Gen 2)) were compared to the baseline date obtained from the reference test.
Location: Centro Jovellanos, Asturias, Spain
Year: October 2013
Number of cases in series: 1
SELECTION OF TESTS
Available measurements: Radiative Flux
SIMULATION SETUP
Grids used: 125 mm
REFERENCES
[1] (2014), Vapour & Fire Control Testing of FOAMGLAS PFS System (Gen 2) on LNG
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Radiative Flux
FUEL N MG VG FAC2 FB NMSE
1 -0.28 0.094
8 6 4
NE/M>n uolro-nE 一 s
ooc^cra> u_-① luo ① o
Geometric mean bias
Experiment [kW/m2]
10.3.4.7 Montoir LNG Pool Fire
METHANE
British Petroleum, Elf Aquitaine, Gaz de France, Shell and Total-CFP have collaborated to perform three LNG fire experiments which have been conducted successfully at Montoir, France, under different wind conditions in a shallow 35 m diameter bund. Large tests were essential to provide suitable data for use in models which would reduce uncertainties in the prediction of very large fires. Three fire tests were performed under different wind conditions during 1987.
Location: Gaz de France, Montoir de Bretagne methane terminal, France
Year: 1987
Number of cases in series: 1
SELECTION OF TESTS
Available measurements: Radiative Flux
SIMULATION SETUP
Grids used: 2187 mm
REFERENCES
spanDELKA and J. Moorhouse and F. TuckerR (1990), The montoir 35m diameter LNG pool fire experiments.
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Radiative Flux
FUEL N MG VG FAC2 FB NMSE
0.32
4.6
^uc^cra> uusluo①0
METHANE
2
1
o o o
3 2 1
NE/M>n 二O*5E_S
4.6
0.33 -1.2
• METHANE
Geometric mean bias
Experiment [kW/m2]
10.3.4.8 Gasoline 0.3m Pool Fire
GASOLINE 0P3M POOL FIRE
BENZENE, N_BUTANE, N_HEXANE, N_PENTANE, N_PROPYLBENZENE, O_XYLENE, TOLUENE
To study the various parameters like burning rate, flame emissivity to further understand the amount of heat flux contributed from flames and its variation with respect to different pool diameters. The experimental setup consists of mild steel circular pans of 2 mm thick and 15 cm height.
Gasoline with mass burning rate of 77 gm/m2.s is considered as fuel for this study. Heat flux is measured at distance equal to pool diameter away from the pool centre on a vertical axis.
The heat flux gauge is traversed along the vertical axis. Location: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY, India
Year: 2013
Number of cases in series: 1
SELECTION OF TESTS
Available measurements: Radiative Flux
SIMULATION SETUP
Grids used: 18 mm
REFERENCES
[1]Siddapureddy, Sudheer (2013), Characterization of Open Pool Fires and Study of Heat Transfer in Bodies Engulfed in Pool Fires
Radiative Flux
FUEL N MG VG FAC2 FB NMSE
BENZENE, N_BUTANE, N_HEXANE, N_PENTANE, N_PROPYLBENZENE, O_XYLENE, TOLUENE 13 1.4 1.2 1 0.37 0.29
IO-1 10° IO1
Geometric mean bias
10 20
Experiment [kW/m2]
• BENZENE, N_BUTANE, N_HEXANE, N_PENTANE, N_PROPYLBENZENE, O_XYLENE, TOLUENE
Table 10.4: Blast validation cases.
10.3.5 Blast
One, medium scale validation case that demonstrates the performance of the FLACS-CFD blast solver are included in the following subsection. Table 10.4 gives a summary of this experiment.
10.3.5.1 Urban Canyon
The objective was to study the blast effects from medium sized high explosive (HE) and thermobaric explosive (TBX) charges detonated in an urban environment. The experiment was scaled 1/5. A simplified urban environment consisting of only four buildings was selected. The buildings were cubic and all dimensions optimized for the purpose of validation of numerical tools. The streets in the urban scenario were chosen to have the same width as the building dimensions, 2.3 meter. Four charge locations and two different heights of burst (0.2, 1.15 m) were used for the explosive charges [1].
Location: Sweden
Year: 2006
Number of cases in series: 8
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 200 mm
REFERENCES
[1]Christensen, S.O. (2009), Urban canyon experiments and numerical calculations, The Norwegian Defence Estates Agency (NDEA). Report number Forsvarsbygg Futura Report 03/2009
FUEL
MG
168
.89
Pressure
VG
FAC2 FB
NMSE
①OUP-」Q> OCSEO^O
10°.
10-1 10° 10
Geometric mean bias
10 20
Experiment [barg]
|
Case name Type Variable Metrics N MG VG FAC2 FB NMSE | ||||||||
|
Flame Acceleration pipe |
Explosion |
Pressure |
12 |
1.7 |
1.4 |
0.67 |
0.53 |
0.36 |
|
silo 12m3 |
Explosion |
Pressure |
8 |
0.52 |
3.6 |
0.5 |
-0.79 |
2.3 |
|
Silo 236m3 |
Explosion |
Pressure |
8 |
4 |
16 |
0.25 |
1 |
2.1 |
|
vented duct 18P5m3 |
Explosion |
Pressure |
60 |
0.35 |
5.9 |
0.38 |
-0.81 |
1.4 |
10.3.6 Dust Explosion
10.3.6.1 Flame Acceleration Pipe
The main aim of this experiment is to study the effect of congestion on dust explosion and determination of the fundamental flame characteristics, in a dust-air mixture and the influence of turbulence on flame propagation. The experimental setup consist of tube with diameter of 0.19 m and with two lengths 1.86 m and 0.93 m with both ends closed. Experiments were conducted with and without obstacles within the tube. Obstacle consist of concentric ring with internal diameter of 114 mm and outside diameter of 165 mm with a spacing of 85 mm. 12 such concentric rings are placed for 1.86m tube and 6 for 0.93 m tube. The ignition is done at the center of the bottom of the tube with ignition energy of 1.75 kJ through out the series of tests. Fuel used is corn starch and experiments are conducted at different ignition delay time and with dust concentration varying from 260 g/m3 to 700 g/m3. (.[1])
Location:
Year:
Number of cases in series: 12
Available measurements: Pressure
Grids used: 10 mm
SELECTION OF TESTS
SIMULATION SETUP
REFERENCES
[1]Yi Kang Pu and Jacek Mazurkiewicz and Jozef Jarosinski and C. {William Kauffman} (1989), Comparative study of the influence of obstacles on the propagation of dust and gas flames, Symposium (International) on Combustion
DATE: FEBRUAR 06, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL N MG VG FAC2 FB NMSE
12
①OUP-」Q> OCSEO^O
10°.
10-1 10° 10
Geometric mean bias
0 8 6 4 2 1'
【ppq】 UOAfu-nlu-s
10.3.6.2 Silo 12m3
The experiments were conducted in cylindrical silo of diameter 1.6m and height 5.6m including bin-hopper at the bottom. The silo bottom was filled with sand to prevent the pressure wave from leaving the silo hence the effective volume was then reduced to 9.4 m3. Corn starch dust cloud was generated using different methods; ring nozzles and pressurized dust reservoirs ('homogeneous cloud'), mechanical feeding, pneumatic dust injection tangentially, and pneumatic dust injection vertically downward. Dust concentrations inside conveying pipe of diameter 75mm, was varied as 1,3,5,7 Kg/m3. The silo has vent openings with polyethylene film (0.1 bar). Four vent areas were used in the campaign 0.15m2,0.3m2,0.5m2 and 0.7m2. The cloud was ignited at three different locations. For the explosion modelling, Silo is assumed to be completely filled with dust cloud.
Location:
Year:
Number of cases in series: 8
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 100 mm
REFERENCES
[1]Skjold, T. and Arntzen, Bjørn and Hansen, Olav and Taraldset, O. and Storvik, Idar and Eckhoff, R. (2005), Simulating Dust Explosions with the First Version of DESC, Process Safety and Environmental Protection
[2]Hauert, F. and Vogl, A. and Radandt, S. (1996), Dust cloud characterization and its influence on the pressure-time-history in silos, Process Safety Progress
[3]F.Hauert, A.Vogl (1995), Measurement of Dust Cloud Characteristics in Industrial Plants1
[4]S.I. Rani and B.A. Aziz and J. Gimbun (2015), Analysis of dust distribution in silo during axial filling using computational fluid dynamics: Assessment on dust explosion likelihood, Process Safety and Environmental Protection
DATE: FEBRUAR 15, 2023 POSTPROCESS QUANTITIES
Pressure
FUEL
MG
VG
FAC2
FB
NMSE
8
2
5 0
2.3
2 1
o o
1 1
①OUB-」(U> util① LUO ① 5
【PQq〕UOAP-nLU-s
0.5 1.0 1.5
Experiment [barg]
10.3.6.3 Silo 236m3
|
SILO 236M3 |
1TK0NC «TML C*l»--- ov*T IKCT. -----n A; HICICST ICNITIM FOIMT- ~—'" ^HtssuRt monc p> { tM/ST CONCCMTRATION__________ J ^xove u, u OUST <VMCtRTR«TIOM MOtC c, ---------- ALTiRMATIVK ---------- ICKITICN SOUKC ll»MTIONS OUST CONCZHTCATION ccvt c« ---■ U 6lH CONCeNTRATIDK Moae c> --------- PR UMM* mom r,, ( ALTEMMTIVl WMmg SOUKS UMMIQM ------ OUST CO«vC,NTflA,IOM none c>------» DUST C<W<<MTMTION FOX C l --------〜 mirssuiie raont,,-- M0«M*L 'BOTTOM icmitiuh' roiKT______£ • .... l.^nABOVe BOTTOM : 。 , a , BOTTOM MukriOM j;"3辰 TUC «a VUTICAL »1»t DRAIN das auuog z mn( —付 CSKSIUCHK *i*m « WHKal axUsi 5 ««*li**al ita |
|
A experimental silo facility, comprising of 236 m3 steel silo cell of height 22 m and diameter with pneumatic dust injection at bottom and top of the silo. The cloud were ignited at various height above the ground. Two vent area of 5.7 m2 and 3.4m2 were used. (.[1]) | |
|
Location: Bergen, Norway Year: December, 1985 Number of cases in series: 8 |
SELECTION OF TESTS
Available measurements: Pressure
SIMULATION SETUP
Grids used: 180 mm
REFERENCES
[2]Skjold, T. and Arntzen, Bjørn and Hansen, Olav and Taraldset, O. and Storvik, Idar and Eckhoff, R. (2005), Simulating Dust Explosions with the First Version of DESC, Process Safety and Environmental Protection
FUEL
MG
Pressure
VG
FAC2
FB
NMSE
2 1
o o
1 1
①OUB-」(U> util① LUO ① 5
.25
2.1
o
Geometric mean bias
5 0 5
1 1 o
【PQq〕co^ra3E-^
1 2
Experiment [barg]
10.3.6.4 Vented Duct 18.5m3
Available measurements: Pressure
SIMULATION SETUP
Grids used: 100 mm
REFERENCES
[1]Diana Castellanos, and Trygve Skjold, and Kees van Wingerden, and Rolf K. Eckhoff, and M. Sam Mannan (2013), Validation of the DESC Code in Simulating the Effect of Vent Ducts on Dust Explosions, Ind. Eng. Chem. Res.
[2]Hey M. (1991), Pressure relief of dust explosions through large diameter ducts and effects of changing the position of the ignition source., J. Loss Prev. Process Ind.
FUEL
N MG
60
5 .3 0
Pressure
VG
.9 5
FAC2
FB
NMSE
山uup-」p> UUJ3E0① 5
1
1
Geometric mean bias
6 4 2 【praq〕UOA-nLU-s
FLACS-CFD v22.2 User’s Manual
GEXCON